20051217029639I

Incident · Minor damage

FAA incident report · Bell 212 · Galveston, TX · December 17, 2005

Date
December 17, 2005 · 16:54 local
Place
Galveston, TX
Airport
Scholes Field Airport
Phase of flight
Sfl Final Approach
Operating rules
General operating rules (Part 91)
Operator
EGIA
Damage
Minor damage
Aircraft
N5410N
Reported as
Bell 212
People aboard
2
Fatal injuries
0
Pilot’s flight hours
13,524 total3,035 in this make and model120 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) During a training flight a #1 hydraulics failure was simulated. The aircraft was at 700 feet MSL, 80 knots and 55% torque when the #1 hydraulics system was turned off. The aircraft immediately experienced a violent, ever-increasing yaw excursions. The afcs was disengaged, all lights out, however yaw excursions continued to increase and the aircraft began violent pitch excursions with corresponding roll motion. The #1 hydraulics system was turned back on and the pitching and yawing started to slow down but did not stop. An emergency was declared and the pilot made a slow turn to line up with the runway at which point the t/r pedal felt as though it was stuck in the left pedal position. At approximately 15 feet the helicopter made a 360 degree uncommanded turn and pitched up. As the aircraft came back around the pilot cut power to both engines and set it down hard. Both cross tubes were bent beyond the limitation. No injuries to the pilots.

As the FAA filed it

(-23) DURING A TRAINING FLIGHT A #1 HYDRAULICS FAILURE WAS SIMULATED. THE AIRCRAFT WAS AT 700 FEET MSL, 80 KNOTS AND 55% TORQUE WHEN THE #1 HYDRAULICS SYSTEM WAS TURNED OFF. THE AIRCRAFT IMMEDIATELY EXPERIENCED A VIOLENT, EVER-INCREASING YAW EXCURSIONS. THE AFCS WAS DISENGAGED, ALL LIGHTS OUT, HOWEVER YAW EXCURSIONS CONTINUED TO INCREASE AND THE AIRCRAFT BEGAN VIOLENT PITCH EXCURSIONS WITH CORRESPONDING ROLL MOTION. THE #1 HYDRAULICS SYSTEM WAS TURNED BACK ON AND THE PITCHING AND YAWING STARTED TO SLOW DOWN BUT DID NOT STOP. AN EMERGENCY WAS DECLARED AND THE PILOT MADE A SLOW TURN TO LINE UP WITH THE RUNWAY AT WHICH POINT THE T/R PEDAL FELT AS THOUGH IT WAS STUCK IN THE LEFT PEDAL POSITION. AT APPROXIMATELY 15 FEET THE HELICOPTER MADE A 360 DEGREE UNCOMMANDED TURN AND PITCHED UP. AS THE AIRCRAFT CAME BACK AROUND THE PILOT CUT POWER TO BOTH ENGINES AND SET IT DOWN HARD. BOTH CROSS TUBES WERE BENT BEYOND THE LIMITATION. NO INJURIES TO THE PILOTS.